FR2967398B1 - STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY - Google Patents

STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY

Info

Publication number
FR2967398B1
FR2967398B1 FR1059392A FR1059392A FR2967398B1 FR 2967398 B1 FR2967398 B1 FR 2967398B1 FR 1059392 A FR1059392 A FR 1059392A FR 1059392 A FR1059392 A FR 1059392A FR 2967398 B1 FR2967398 B1 FR 2967398B1
Authority
FR
France
Prior art keywords
turbojet
strengthening
capacity
turbojet capacity
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR1059392A
Other languages
French (fr)
Other versions
FR2967398A1 (en
Inventor
Pierre Caruel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR1059392A priority Critical patent/FR2967398B1/en
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to BR112013010654A priority patent/BR112013010654A2/en
Priority to EP11802464.5A priority patent/EP2640639B1/en
Priority to RU2013126748/11A priority patent/RU2569725C2/en
Priority to CN201180054683.3A priority patent/CN103209893B/en
Priority to PCT/FR2011/052564 priority patent/WO2012066211A1/en
Priority to CA2816455A priority patent/CA2816455A1/en
Publication of FR2967398A1 publication Critical patent/FR2967398A1/en
Application granted granted Critical
Publication of FR2967398B1 publication Critical patent/FR2967398B1/en
Priority to US13/894,647 priority patent/US10087842B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1059392A 2010-11-16 2010-11-16 STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY Expired - Fee Related FR2967398B1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1059392A FR2967398B1 (en) 2010-11-16 2010-11-16 STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY
EP11802464.5A EP2640639B1 (en) 2010-11-16 2011-11-03 Turbojet engine nacelle reinforcing structure
RU2013126748/11A RU2569725C2 (en) 2010-11-16 2011-11-03 Turbojet engine nacelle reinforcing structure
CN201180054683.3A CN103209893B (en) 2010-11-16 2011-11-03 Turbojet engine nacelle strengthens structure
BR112013010654A BR112013010654A2 (en) 2010-11-16 2011-11-03 turbojet engine compartment comprising a fixed structure
PCT/FR2011/052564 WO2012066211A1 (en) 2010-11-16 2011-11-03 Turbojet engine nacelle reinforcing structure
CA2816455A CA2816455A1 (en) 2010-11-16 2011-11-03 Turbojet engine nacelle reinforcing structure
US13/894,647 US10087842B2 (en) 2010-11-16 2013-05-15 Turbojet engine nacelle reinforcing structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1059392A FR2967398B1 (en) 2010-11-16 2010-11-16 STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY

Publications (2)

Publication Number Publication Date
FR2967398A1 FR2967398A1 (en) 2012-05-18
FR2967398B1 true FR2967398B1 (en) 2012-11-02

Family

ID=44149010

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1059392A Expired - Fee Related FR2967398B1 (en) 2010-11-16 2010-11-16 STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY

Country Status (8)

Country Link
US (1) US10087842B2 (en)
EP (1) EP2640639B1 (en)
CN (1) CN103209893B (en)
BR (1) BR112013010654A2 (en)
CA (1) CA2816455A1 (en)
FR (1) FR2967398B1 (en)
RU (1) RU2569725C2 (en)
WO (1) WO2012066211A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9404507B2 (en) * 2013-04-15 2016-08-02 Mra Systems, Inc. Inner cowl structure for aircraft turbine engine
FR3009339B1 (en) * 2013-07-30 2018-01-26 Safran Aircraft Engines TURBOMACHINE COMPRISING A PYLON COOLING DEVICE
US9771894B2 (en) 2013-10-07 2017-09-26 Rohr, Inc. Radially connected cascade grids
FR3047973B1 (en) * 2016-02-23 2018-03-09 Airbus Operations AIRCRAFT ENGINE ASSEMBLY, COMPRISING A MOTOR ATTACHING DEVICE EQUIPPED WITH STRUCTURAL MOBILE HOOKS CONNECTED TO THE CENTRAL CABIN
FR3065710A1 (en) * 2017-04-27 2018-11-02 Airbus Operations METHOD FOR CALIBRATION BY MEASURING THE RIGIDITY OF SUPPORT STRUCTURES OF A MODEL COMPRISING A MAIN STRUCTURE AND AT LEAST ONE SUPPORT STRUCTURE
FR3075886B1 (en) * 2017-12-22 2019-12-27 Safran Nacelles TURBOREACTOR NACELLE HAVING HOOD OPENINGS BEFORE ACCESS TO NACELLE FIXING POINTS
FR3088373B1 (en) * 2018-11-09 2021-03-19 Safran Nacelles GASKET FOR AIRCRAFT TURBOREACTOR NACELLE
FR3096741B1 (en) * 2019-05-28 2022-11-18 Safran Nacelles Aircraft propulsion system
US11268406B2 (en) * 2019-08-12 2022-03-08 The Boeing Company Movement-limiting device for a turbine engine and associated method
CN113928573B (en) * 2021-11-19 2023-04-18 中国直升机设计研究所 Sliding fairing with guiding and buffering functions

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3500646A (en) * 1968-04-19 1970-03-17 Rohr Corp Thrust reverser
GB1583952A (en) * 1976-07-13 1981-02-04 Short Brothers & Harland Ltd Gas turbine engines
US5046689A (en) * 1989-04-19 1991-09-10 The Boeing Company Cowling interlock system
FR2762875B1 (en) * 1997-04-30 1999-06-04 Hispano Suiza Sa PROTECTED DRIVE INVERTER IN THE EVENT OF ACCIDENTAL UNLOCKING
FR2856379B1 (en) * 2003-06-18 2006-11-24 Airbus France AIRCRAFT ENGINE HAVING BLOWER HOUSINGS AND THRUST INVERTERS SEPARATED BY REDUCED GAME
FR2896481B1 (en) * 2006-01-23 2009-12-04 Aircelle Sa FIXING SYSTEM FOR COMPONENT ELEMENT OF A TURBOJET CAPACITY
US8523516B2 (en) * 2006-10-11 2013-09-03 Aircelle Bypass turbojet engine nacelle
FR2908152B1 (en) * 2006-11-08 2009-02-06 Snecma Sa TURBOMACHINE TURBINE BOW
FR2915527B1 (en) * 2007-04-30 2009-06-12 Aircelle Sa REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER
FR2925607B1 (en) * 2007-12-21 2013-05-10 Aircelle Sa NACELLE FOR AIRCRAFT ENGINE WITH VARIABLE SECTION TUBE
RU2509649C1 (en) * 2012-11-01 2014-03-20 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Method of making aircraft thrust reverser bearing grate sections from polymer composites, mandrel to this end, mould for pouring anti-adhesion elastic material of mandrel separation layer for implementation of said method and sections of aircraft thrust reverser bearing grate

Also Published As

Publication number Publication date
EP2640639B1 (en) 2015-12-30
BR112013010654A2 (en) 2016-08-09
FR2967398A1 (en) 2012-05-18
RU2013126748A (en) 2014-12-27
CN103209893A (en) 2013-07-17
US10087842B2 (en) 2018-10-02
CA2816455A1 (en) 2012-05-24
RU2569725C2 (en) 2015-11-27
CN103209893B (en) 2015-08-12
WO2012066211A1 (en) 2012-05-24
EP2640639A1 (en) 2013-09-25
US20130243589A1 (en) 2013-09-19

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Year of fee payment: 6

ST Notification of lapse

Effective date: 20170731